N339SW

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 74,115 hrs · 65,851 cycles

AIR TURNBACK/DECLARED EMERGENCY. NR 2 ENGINE DRIVEN LOW HYDRAULIC PRESSURE LIGHT FLICKERING WITH ASSOCIATED FLUCTUATING PRESSURE INDICATION. REMOVED AND REPLACED NR 2 ENGINE DRIVEN PUMP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,934 hrs · 65,709 cycles

DURING SCHEDULED SPV CHECK, FOUND LT STUB FRAME CRACKED AT BS 597. REMOVED AND REPLACED FRAME PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 72,574 hrs · 64,689 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 23. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 72,275 hrs · 64,449 cycles

LEFT OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17. SECURED LENS PER MM.

Part: BATTERY PACK — DISCONNECTED (CABIN) · airframe 72,224 hrs · 64,408 cycles

DURING SCHEDULED 22Y CHECK, FOUND EEPLS INOP. RECONNECTED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,224 hrs · 64,408 cycles

DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 344, STR 23L. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 662, RBL 24.5. REPAIRED CHORD PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 328, STR 20R. REPAIRED WEB PER SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, LBL 45.5. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 320, STR 20L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL WEB CRACKED AT BS 708.5, RBL 24.5. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 24.5. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 668, LBL 24.5. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 668, RBL 24.5. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 336, STR 20L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, LBL 24.5. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 51. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 672, LBL 24.5. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 706, LBL 24.5. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, RBL 24.5. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 665, LBL 24.5. REPAIRED BEAM PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 10L STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,206 hrs · 64,392 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM AND EA.

Part: LIGHT — BROKEN (CABIN) · airframe 71,914 hrs · 64,163 cycles

R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,889 hrs · 64,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EEPLS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 71,724 hrs · 64,016 cycles

AT FL 360 R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 71,334 hrs · 63,705 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 71,071 hrs · 63,502 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,323 hrs · 62,930 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,323 hrs · 62,930 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,226 hrs · 62,853 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,043 hrs · 62,722 cycles

AFT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,849 hrs · 62,583 cycles

DURING SCHEDULED HC2 CHECK, FOUND KEEL BEAM CORRODED AT BS 508C, STR 28R. REPAIRED BEAM PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,849 hrs · 62,583 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CORRODED AT BS 508C, STR 28R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 70,549 hrs · 63,519 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EVAC SLIDE LOOSE. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,203 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING DOOR LOWER EXIT LIGHT INOP. RELAMPED PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, BETWEEN STR 13R TO STR 14R. REPAIRED SHEAR TIE PER ER.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 25R. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN DISBONDED AT BS 360, BETWEEN STR 8R TO STR 9R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727D, BETWEEN STR 19R TO STR 20R. REPAIRED SHEAR TIE PER BAC DWG.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN DISBONDED AT BS 908, STR 10R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 1006, BETWEEN STR 24L TO STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 400 TO BS 420, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 867 TO BS 887, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 308, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 907 TO BS 967, BETWEEN STR 25R TO STR 25L. REMOVED AND REPLACED SKIN PANEL PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,204 hrs · 62,060 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 1R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,094 hrs · 61,978 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,904 hrs · 61,830 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT 727C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,904 hrs · 61,830 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,800 hrs · 61,751 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,739 hrs · 61,706 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 984, STR 21L. REPAIRED SKIN PER SWA EA.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 68,737 hrs · 61,705 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD MOUNT CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,737 hrs · 61,705 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 984, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 68,499 hrs · 61,529 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,394 hrs · 61,450 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,214 hrs · 61,335 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 470, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,884 hrs · 61,106 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,884 hrs · 61,106 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 790, STR 17L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,884 hrs · 61,106 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: GROUND STUD — DEFECTIVE (CABIN) · airframe 67,018 hrs · 60,484 cycles

DURING SCHEDULED 20Y CHECK, FOUND FIRST RT OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED EXIT LIGHT ELECTRIC GROUND STUD PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,008 hrs · 60,477 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERIES PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,008 hrs · 60,477 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERIES PER MM.

Part: TAB — CORRODED (LT AILERON) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT AILERON TAB CORRODED AT HINGE DOUBLER UPPER SURFACE. REMOVED AND REPLACED TAB PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING LEADING EDGE NR 3 SLAT I/B UPPER WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER AAR EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING L/E NR 3 SLAT INBOARD UPPER WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CRACKED AT BS 1016, STR 8R. REPAIRED BULKHEAD PER AAR EA.

Part: LIGHT — NOT SEATED (CABIN) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT RT OVERHEAD EMERGENCY EXIT LIGHT INOP. RESEATED LIGHT PER MM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MAIN GEAR W/W FWD PRESSURE BULKHEAD CRACKED NEXT TO AILERON CONTROL SHAFT. REPAIRED WEB PER AAR EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CRACKED AT BS 1016, STR 6R. REPAIRED BULKHEAD PER AAR EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD BULKHEAD O/B STIFFENER CRACKED AT BS 663, RBL 6.15. REPLACED STIFFENER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUOUT BELOW FWD END OF HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT JUST ABOVE FWD END OF HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING O/B FLAP, AFT FLAP DELAMINATED AT INBOARD END ALONG T/E. REPAIRED FLAP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 787, BETWEEN RBL 10 AND RBL 19. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 291, STR 16R. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, RBL 42. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 947.5, RBL 2 TO LBL 4. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER OPENING CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 360, STR 15L. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 410, RBL 2. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 430, RBL 2. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 390, LBL 4. REPAIRED SKIN PER AAR EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR AFT CUTOUT FRAME CRACKED AT SECOND STOP FITTING. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 L-ANGLE STRINGER FWD OF GALLEY SERVICE DOOR CRACKED AT BS 294.5, STRINGER 17R. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, RBL 65. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827 STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S24L) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727C S21R) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S25L) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S23R) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S22R) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S21R) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S22R) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727A S8L) · airframe 66,977 hrs · 60,461 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,394 hrs · 60,026 cycles

DURING SCHEDULED C2 CHECK, FOUND STRINGER 16L CRACKED AT BS 517. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,724 hrs · 59,523 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 21R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,724 hrs · 59,523 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SWA EA.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 65,452 hrs · 59,317 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,452 hrs · 59,317 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,820 hrs · 58,853 cycles

DURING SCHEDULED A1 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 64,453 hrs · 58,579 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 64,443 hrs · 58,573 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,443 hrs · 58,573 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,443 hrs · 58,573 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (NR 1 SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND LT WING NR 1 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 6 SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 6 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SPOILER — DELAMINATED (LH WING) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND LT WING NR 2 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 3 SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND LT WING NR 3 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND LEFT WING 0 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 7 SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 7 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 8 SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND RIGHT WING NR 8 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 64,048 hrs · 58,268 cycles

DURING SCHEDULED A2 CHECK, FOUND RT WING NR 5 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,506 hrs · 57,851 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 5. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,486 hrs · 57,834 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,486 hrs · 57,834 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,486 hrs · 57,834 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,224 hrs · 57,623 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,224 hrs · 57,623 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,828 hrs · 57,317 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,812 hrs · 57,304 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 924 S23L) · airframe 62,253 hrs · 56,858 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,686 hrs · 56,437 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 19R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,686 hrs · 56,437 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT T/E OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: ATTACH FITTING — BROKEN (NR 4 SPOILER) · airframe 61,686 hrs · 56,437 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING NR 4 GROUND SPOILER OUTBOARD ACTUATOR ATTACH POINT BROKEN ON SPOILER SIDE. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,686 hrs · 56,437 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 550, STR 15R. REPAIRED SKIN PER SWA EA.

Part: CONTROLLER — FAILED (COCKPIT WINDOW) · airframe 61,021 hrs · 55,934 cycles

FLIGHT COMPT L2 WINDOW ARCHED AT LOWER FWD CORNER. REMOVED AND REPLACED L2 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 61,004 hrs · 55,920 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,685 hrs · 55,691 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 60,685 hrs · 55,691 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 59,720 hrs · 54,929 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 12 DEF TO ROW 14 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,821 hrs · 54,232 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: CABLE ASSY — MISROUTED (L2 DOOR SLIDE) · airframe 58,797 hrs · 54,210 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT INOP BETWEEN ROW 16 TO ROW 17. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 500C) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 21R. REPAIRED SKIN PER SWA EA.

Part: CONTAINER — CRACKED (L1 DOOR SLIDE) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CONTAINER CRACKED AT GIRT BAR RETAINING BRACKET. REMOVED AND REPLACED SLIDE CONTAINER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELT FRAME CRACKED AT BS 616, LBL 65. REPAIRED BELT FRAME PER SWA SRM.

Part: FLOORBEAM — CRACKED (BS 663) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (BS 500B) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 21L. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CORRODED (BS 500D) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 500D, RBL 8. REPAIRED KEEL BEAM PER SRM.

Part: SKIN — CRACKED (BS 515D) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 16R. REPAIRED SKIN PER SRM.

Part: TAB — DELAMINATED (RT WING AILEORN) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED TAB PER MM.

Part: FRAME — CRACKED (BS 500B) · airframe 58,677 hrs · 54,112 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 21R. REPAIRED FRAME PER SWA EA & SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 58,097 hrs · 53,660 cycles

DURING SCHEDULED A1 CHECK, FOUND L1 DOOR INTERIOR & EXTERIOR EMERGENCY EXIT LIGHTS INOP. SECURED BATTERY PACK PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,905 hrs · 53,505 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,952 hrs · 52,777 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945.5, STR 25R. REPAIRED SKIN PER SWA EA & SRM.

Part: HOOK — OUT OF POSITION (R2 DOOR) · airframe 56,922 hrs · 52,752 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS OUT OF POSITION. REPOSITIONED HOOKS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 55,998 hrs · 52,033 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LOCK RING — MISSING (L1 DOOR) · airframe 55,996 hrs · 52,032 cycles

L1 DOOR WOULD NOT OPEN. INSTALLED UPPER GUIDE ARM LOCK RING PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 55,536 hrs · 51,675 cycles

DURING SCHEDULED RON CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 53,655 hrs · 50,205 cycles

R2 DOOR EVAC SLIDE GIRT BAR AFT DOOR HOOK LOOSE. SECURED AFT GIRT BAR HOOK PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,390 hrs · 49,981 cycles

DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: HOOK — CORRODED (R1 DOOR GIRT BAR) · airframe 53,371 hrs · 49,963 cycles

DURING SPV, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS, CORRODED. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,371 hrs · 49,963 cycles

DURING SPV, FOUND FRAME AT BS 380, STRINGER 15R, STRINGER 16R, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 53,371 hrs · 49,963 cycles

DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (BS 360) · airframe 53,371 hrs · 49,963 cycles

DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,371 hrs · 49,963 cycles

DURING SPV, FOUND SHEAR TIE AT BS 420, STRINGER 10R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,371 hrs · 49,963 cycles

DURING SPV, FOUND FRAME AT BS 520, STRINGER 12L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 32,451 hrs · 27,995 cycles

DURING SPV, FOUND STRINGER SPLICE AT BS 908, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,451 hrs · 27,995 cycles

DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,451 hrs · 27,995 cycles

DURING SPV, FOUND BUTT STRAP AT BS 908, STRINGER 4R, CRACKED. REPAIRED STRAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,166 hrs · 49,797 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 917 AND BS 924, STR 23R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 53,157 hrs · 49,787 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 52,213 hrs · 49,023 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: BULKHEAD — CRACKED (LT MLG W/W) · airframe 50,574 hrs · 47,684 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD BEADED WEB CRACKED AT BS 664, LBL 31. REPAIRED BEADED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,574 hrs · 47,684 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR CUTOUT FWD UPPER CORNER. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,574 hrs · 47,684 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 13R AND STR 14R. REPAIRED FRAME PER SRM.

Part: GUSSET — CRACKED (FWD SVC DOOR) · airframe 50,574 hrs · 47,684 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER GUSSET CRACKED AT OUTBD FASTENER. REPAIRED AFT LOWER GUSSET PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,574 hrs · 47,684 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT LONGITUDINAL FLOORBEAM CORRODED AT BS 860, LBL 8. REPAIRED BEAM PER SRM AND SWA EA.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 50,519 hrs · 47,629 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM.

Part: THRESHOLD — LEAKING (FUSELAGE) · airframe 49,477 hrs · 46,807 cycles

CABIN ALTITUDE ALERT HORN SOUNDED, EMERGENCY DESCENT TO 9,000 FT, NO MASKS WERE DEPLOYED. FOUND EXCESSIVE LEAK AT AFT CARGO DOOR THRESHOLD. REMOVED THRESHOLD, RESEALED & REINSTALLED PER MM. CONFIDENCE CHECK PASSED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,538 hrs · 46,034 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 556, STR 10R. REPAIRED SKIN PER SRM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 47,550 hrs · 45,237 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB CRACKED AT HINGE CUTOUTS. REMOVED AND REPLACED LT ELEVATOR TAB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,601 hrs · 44,462 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 969 AND BS 971, AT STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,601 hrs · 44,462 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 935, ABOVE STR 24R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 46,236 hrs · 44,171 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER SRM.

Part: TAB — WORN (ELEVATOR) · airframe 46,236 hrs · 44,171 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,803 hrs · 43,803 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT 2.5 INCHES AT BS 940, STR 24R. REPAIRED SKIN PER SRM.

Part: VANE — BENT (AOA) · airframe 45,770 hrs · 43,781 cycles

AIR TURNBACK, CAPT'S STALL WARNING CONTROL COLUMN ACTIVATED. FOUND AOA VANE BENT. REMOVED AND REPLACED AOA VANE PER MM.

Part: BULKHEAD — BUCKLED (FUSELAGE) · airframe 44,936 hrs · 43,072 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT PRESS BULKHEAD BUCKLED, BS 1016, STRINGER 7L AND STRINGER 14L. REPAIRED BULKHEAD WEB AND STRAP PER SWA RA 1-353-2763 AND SRM.

Part: RING — DETERIORATED (FWD ENTRY DOOR) · airframe 44,062 hrs · 42,364 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE RELEASE LATCH ASSY SPLIT RING SOLDER DETERIORATED. RESOLDERED SPLIT RING PER MM.

Part: BEARING — WORN (LH WING) · airframe 44,062 hrs · 42,364 cycles

DURING SCHEDULED C2 CHECK, FOUND PLAY AT LH AILERON HINGES. R&R BEARINGS AT # 1, 2 & 4 HINGES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,355 hrs · 41,751 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT BOTH OVERWING EXITS. RELAMPED EXIT LIGHTS PER MM.

Part: BEAM — CRACKED (BULKHEAD) · airframe 42,568 hrs · 41,082 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA. BS 178 BULKHEAD VERTICAL BEAM CRACKS AT LBL 5.7, INBD & OUTBD RADIUS, WL 184.REPAIRED VERTICAL BEAM PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 42,568 hrs · 41,082 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L/H KEEL BEAM FLANGE CORRODED AT BS 500D+2, OUTBD SURFACE. REPAIRED KEEL BEAM PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,568 hrs · 41,082 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKS AT LBL 17.1, WL 226 & RBL 17.1, AT RETAINER HOLE, 3 ABOVE LOWER EDGE OF BEAM. REPAIRED VERTICAL BEAM WEBS PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,568 hrs · 41,082 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR UPPER FWD CUTOUT. REPAIRED SKIN PER BAC SB.

Part: CONTROLLER — LOOSE (CABIN PRESSURE) · airframe 42,541 hrs · 41,062 cycles

AIR TURNBACK, CABIN CLIMBED NORMAL TO 1000 FT THEN ABRUPTLY CLIMBED AND RETURNED TO NORMAL. AT 15,000 FT, CABIN DEPRESSURIZED, NO HELP IN STANDBY OR NORMAL MODE. FOUND CABIN PRESS CONTROLLER LOOSE IN RACK. SECURED CONTROLLER AND PRESSURIZED AIRCRAFT PER MM. OPS CHECK GOOD. PERFORMED PACK CONFIDENCE CHECK PER SWA SAM 728.

Part: LENS — LOOSE (CABIN) · airframe 42,171 hrs · 40,755 cycles

DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,759 hrs · 40,398 cycles

DURING SCHEDULED A2 CHECK, FOUND 3.0 EXTERNAL FUSELAGE SKIN CRACK AT BS 927, STR 22L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 41,351 hrs · 40,060 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE IND SHOWS LOW PRESS. R&R SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,180 hrs · 39,916 cycles

DURING SCHEDULED C3 CHECK, FOUND 1.5 EXTERNAL FUSELAGE SKIN CRACK AT BS 520, STR 12L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 39,820 hrs · 38,735 cycles

AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. R & R SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,389 hrs · 38,364 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT FWD END. SECURED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RT FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — CONTAMINATED (CABIN)

DURING SCHEDULED C2 CHECK, FOUND MOISTURE INSIDE EMERGENCY LIGHT LENS ON AFT ENTRY DOOR AREA. REMOVED, CLEANED, AND RESEALED LENS AT LIGHT.

Part: LIGHT — INOP (MID CABIN)

DURING SCHEDULED C2 CHECK, FOUND LT EMERGENCY EXIT OVERWING DOOR LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED BC1 CHECK, FOUND FLOOR PROXIMITY LIGHTING TRACK LOOSE FWD OF AFT GALLEY. REATTACHED TRACK PER MM.

Part: OUTFLOW VALVE — OBSTRUCTION (CABIN)

AIR TURNBACK, DURING TAKEOFF, PRESSURIZATION AUTO FAIL LIGHT CAME ON, NO PRESSURIZATION CAPABILITY AT ALL. DISCOVERED A PLASTIC TUBING DEBRIS OBSTRUCTING THE OUTFLOW VALVE TRAVEL. REMOVED OBSTRUCTION, PRESSURIZED AIRCRAFT, OPS CHECKED GOOD PER MM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED IN LOWER AFT CORNER APPROX .375 INCH. REPAIRED PER BOEING SRM.

Part: TARGET — OUT OF ADJUST (CARGO DOOR)

TAKEOFF ABORTED AT 75KTS INDICATED. TAKEOFF ABORTED DUE TO AFT CARGO LIGHT ILLUMINATED. OPC INDICATES 10.9 MILLION FT LBS/24 MINUTE BRAKE COOLING. ADJUSTED AFT CARGO DOOR TARGET AND OPS CKD OK PER BOEING MM.

Part: TIP — CORRODED (VERT STAB)

DURING SCHEDULED D-CHECK, FOUND VERT FIN CENTER TIP FAIRING HAS WING CORRODED AT FASTENER HOLES AND FWD EDGE. REPAIRED L/E VERT STAB PER BOEING SRM.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 727, LBL 65.25, WL 232 ADJACENT TO STR 14L. REPAIRED PER TRAMCO ER NR 98-0921A.

Part: FITTING — CORRODED (NR 5 LE SLAT ACT)

DURING SCHEDULED D-CHECK, FOUND CORRODED NR 5 SLAT ACTUATOR FITTING, I/B RIB HAS A PITTING CORRODED IN ROD END ATTACH HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 857)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 857, RBL 7.5 UPPER SURFACE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS PER BOEING SRM.

Part: CLIP — CRACKED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND L-CLIP CRACKED, SUPPORT BRACKET TOP OF NR 1 PYLON. REMOVED AND REPLACED PER BOEING SRM.

Part: COVERPLATE — DAMAGED (BS 794.5)

DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME COVERPLATE AT BS 794.5, RBL 30 DAMAGED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED D CHECK, FOUND CRACKED NR 6 SLAT LWR SKIN AT CENTER AUX TRACK. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER 16 RT AT BS 500C +4.0. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D CHECK, FOUND CRACKED FWD SERVICE DOOR FWD LWR STUB FRAME AT BS 296, RBL 60, WL 209. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D CHECK, FOUND CRACKED LWR FWD HINGE CUT OUT ON FSD. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 771)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, RBL 8.10, WL 159. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 277)

DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 277, STR 15R. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 907, RBL 2, WL 303. REPAIRED PER BOEING SRM.

Part: FRAME — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME COVERPLATE AT BS 847, RBL 30 DAMAGED. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 771)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, LBL 3, WL 159. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 907 BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO NR 98-0896.

Part: ANGLE — CHAFED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E L- ANGLE AND STIFFENER ARE CHAFFED AT LWR SIDE OF FLAP CUTOUT. REMOVED AND REPLACED PER BOEING SRM.

Part: BRACKET — CRACKED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E L BRACKET SUPPORT CRACKED AT UPPER OF FLAP CUTOUT ON AFT PANEL SUPPORT. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 867)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 867 BETWEEN STR 8 AND 9 RT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: FRAME — CRACKED (BS 380)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 380 BETWEEN STR 8 & 9 LT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: FRAME — CRACKED (BS 480)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 480 BETWEEN STR 8 & 9 RT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E LWR SIDE ANGLE SUPPORT CRACKED JUST FWD OF TAILCONE FITTING. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 400 BETWEEN STR 8 & 9 RT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: FRAME — CRACKED (BS 400)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 400 BETWEEN STR 8 & 9 LT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 500A BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 440 BETWEEN STR 8 & 9 RT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: FRAME — CRACKED (BS 867)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 867 BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: BRACKET — GOUGED (NR 1 PYLON)

DURING SCHEDULED D CHECK, FOUND NR 1 PYLON SPRING DOOR AND MOUNT BRACKET IS GOUGED. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 480)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 480 BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO ER NR 98-0896.

Part: INTERCOSTAL — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND INTERCOSTAL AT BS 727A TO 727B, RBL 25, WL 158 CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 771)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, LBL 8.10, WL 159. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 304)

DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 304 BETWEEN STR 27-28 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 771)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, RBL 3, WL 159. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 775-857)

DURING SCHEDULED D CHECK, FOUND CORRODED TIE STRAP AT BS 775-857, WL 156, RBL 19. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 500)

DURING SCHEDULED D CHECK, FOUND INTERCOSTAL AT BS 500 TO 500A, LBL 25, WL 158 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 358)

DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 358 ABOVE STR 22R. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 180)

DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 180, WL 207, RBL 27 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CORRODED (BS 947.5)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 947.5 RBL 20, LBL 20. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 200. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 6.7, WL 212.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 198.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 201. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 4.7, WL 212.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED UNDER STRAP AT LBL 4.7, WL 201. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 5.7, WL 201. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 02, WL 207. REMOVED AND REPLACED PER TRAMCO ER 98-0891.

Part: STRAP — CORRODED (BS 500)

DURING SCHEDULED D CHECK, FOUND CORRODED FWD CARGO PIT FLOOR SUPPORT STRAP AT BS 500+4, LBL 13, LBL 15.5, WL 156.5. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — WORN (BS 860-887)

DURING SCHEDULED D CHECK, FOUND SKIN WEAR COMMON TO DORSAL FIN AT BS 860-887, WL 306.5. ACCOMPLISHED REPAIR PER ACO NR 6738-55.

Part: WEB — CORRODED (BS 296)

DURING SCHEDULED D CHECK, FOUND CORRODED FWD SERVICE DOOR FLOOR WEB AT BS 296, RBL 56, WL 208.5. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 180)

DURING SCHEDULED D CHECK, FOUND FLOOR WEB BS 180, WL 207, RBL 27 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 312)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 312 DAMAGED FASTENER HOLES ON VERTICAL WEB FROM LBL 16 TO RBL 8, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 1006)

DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 1006, LBL 39, WL 208. REPAIRED PER BOEING SRM.

Part: BRACKET — CORRODED (LANDING GEAR)

DURING SCHEDULED D CHECK, FOUND LT STABILIZER LINK LOWER PANEL L BRACKET CORRODED. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 1010-1013)

DURING SCHEDULED D CHECK, FOUND TWO GOUGES ON FUSELAGE SKIN AT BS 1010 AND 1013, 2 BELOW STR 11R. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (BS 486)

DURING SCHEDULED D CHECK, FOUND FWD CARGO BAY AFT DOOR FRAME COVER PLATE WEB DAMAGED AT BS 486, WL 158, RBL 26. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (BS 344)

DURING SCHEDULED D CHECK, FOUND FWD CARGO BAY AFT DOOR FRAME COVER PLATE WEB DAMAGED AT BS 344, RBL 26, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 994)

DURING SCHEDULED D CHECK, FOUND CORRODED OUTBOARD CHORD ANGLE ON THRESHOLD AT BS 994, RBL 51, WL 208.

Part: INTERCOSTAL — CRACKED (BS 380-400)

DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CRACKED AT BS 380-400, WL 208, BL 0. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 360)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM DAMAGED AT NUTPLATE BS 360, WL 208, RBL 52. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 344)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM DAMAGED AT NUTPLATE BS 344, WL 208, LBL 28-48. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND OF BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 6.7, WL 212. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 1015)

DURING SCHEDULED D CHECK, FOUND CORRODED INTERCOSTAL AT BS 1015, LBL 37, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 326.5)

DURING SCHEDULED D CHECK, FOUND INTERCOSTAL WEB CRACKED AT BS 326.5, LBL 45, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 312)

DURING SCHEDULED D CHECK, FOUND DAMAGED AT NUTPLATE LOCATIONS BS 312, RBL 1-12, WL 208 ON FLOORBEAM UPPER CHORD. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED D CHECK, FOUND FWD GALLEY SERVICE DOORWAY CRACKED AT SKIN CUTOUT LOWER AFT CORNER. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — CRACKED (BS 312)

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL STRAP CRACKED AT WL 200, LBL 10 BS 312. REPAIRED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540, RBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD SIDE CHORD RT SIDE CRACKED AT WL 207. REPAIRED PER BOEING SRM.

Part: STRAP — CRACKED (BS 314.5)

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL STRAP CRACKED AT BS 314.5, RBL 33, WL 200. REMOVED AND REPLACED PER BOEING SRM.

Part: MOUNT — CORRODED (BS 1012)

DURING SCHEDULED D CHECK, FOUND CORRODED AFT LAV MOUNT AT BS 1012, LBL 38, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — CORRODED (BS 1016)

DURING SCHEDULED D CHECK, FOUND CORRODED STRAP AT BS 1016, LBL 3, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 986, LBL 14, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL .5, RBL .5, WL 187. REPAIRED PER BOEING SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD SIDE CHORD LT SIDE CRACKED AT WL 207. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 397)

DURING SCHEDULED D CHECK, FOUND DENTED FUSELAGE SKIN AT BS 397, 2 BELOW STRINGER 15L. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AROUND FASTENER LOCATIONS AT BS 328, WL 208, RBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 312)

DURING SCHEDULED D CHECK, FOUND INTERCOSTAL WEB CRACKED AT FASTENER LOCATION BS 312, RBL 1.5, WL 208. REPAIRED PER BOEING SRM.

Part: SKIN — CORRODED (BS 500)

DURING SCHEDULED D CHECK, FOUND PREVIOUS BLEND OUT SKIN AT BS 500B+29, LBL 14, WL 304. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 964)

DURING SCHEDULED B/C4 CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 964, NEAR S24L. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 203/927)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 927, S19L, AND AT BS 203, ABOVE E/E DOOR. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4 D-CHECK, FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT FWD UPPER RADIUS OF DOOR TORQUE TUBE CUTOUT, AT AFT SERVICE DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD UPPER RADIUS OF TORQUE TUBE CUTOUT AT AFT SERVICE DOOR. REPAIRED PER BOEING SRM.